GB0003029D0 - A method of reinforcing a laminated member such as a skin for an aircraft - Google Patents

A method of reinforcing a laminated member such as a skin for an aircraft

Info

Publication number
GB0003029D0
GB0003029D0 GBGB0003029.6A GB0003029A GB0003029D0 GB 0003029 D0 GB0003029 D0 GB 0003029D0 GB 0003029 A GB0003029 A GB 0003029A GB 0003029 D0 GB0003029 D0 GB 0003029D0
Authority
GB
United Kingdom
Prior art keywords
skin
reinforcing
aircraft
laminated
laminated member
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
GBGB0003029.6A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by British Aerospace PLC filed Critical British Aerospace PLC
Priority to GBGB0003029.6A priority Critical patent/GB0003029D0/en
Publication of GB0003029D0 publication Critical patent/GB0003029D0/en
Priority to ES01905863T priority patent/ES2202274T3/es
Priority to AT01905863T priority patent/ATE249921T1/de
Priority to US10/182,904 priority patent/US7780808B2/en
Priority to AU2001233835A priority patent/AU2001233835A1/en
Priority to DE60100802T priority patent/DE60100802T2/de
Priority to EP01905863A priority patent/EP1263572B1/fr
Priority to PCT/GB2001/000469 priority patent/WO2001058680A1/fr
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B32B3/08—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24752—Laterally noncoextensive components

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
GBGB0003029.6A 2000-02-11 2000-02-11 A method of reinforcing a laminated member such as a skin for an aircraft Ceased GB0003029D0 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
GBGB0003029.6A GB0003029D0 (en) 2000-02-11 2000-02-11 A method of reinforcing a laminated member such as a skin for an aircraft
ES01905863T ES2202274T3 (es) 2000-02-11 2001-02-06 Un metodo para reforzar un miembro estratificado tal como un revestimiento para un avion.
AT01905863T ATE249921T1 (de) 2000-02-11 2001-02-06 Verfahren zur verstärkung eines laminats z.b für die aussenhaut von flugzeugen
US10/182,904 US7780808B2 (en) 2000-02-11 2001-02-06 Method of reinforcing a laminated member such as a skin for an aircraft
AU2001233835A AU2001233835A1 (en) 2000-02-11 2001-02-06 A method of reinforcing a laminated member such as a skin for an aircraft
DE60100802T DE60100802T2 (de) 2000-02-11 2001-02-06 Verfahren zur verstärkung eines laminats z.b für die aussenhaut von flugzeugen
EP01905863A EP1263572B1 (fr) 2000-02-11 2001-02-06 Procede de renforcement d'un produit stratifie, notamment un revetement d'avion
PCT/GB2001/000469 WO2001058680A1 (fr) 2000-02-11 2001-02-06 Procede de renforcement d'un produit stratifie, notamment un revetement d'avion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0003029.6A GB0003029D0 (en) 2000-02-11 2000-02-11 A method of reinforcing a laminated member such as a skin for an aircraft

Publications (1)

Publication Number Publication Date
GB0003029D0 true GB0003029D0 (en) 2000-03-29

Family

ID=9885293

Family Applications (1)

Application Number Title Priority Date Filing Date
GBGB0003029.6A Ceased GB0003029D0 (en) 2000-02-11 2000-02-11 A method of reinforcing a laminated member such as a skin for an aircraft

Country Status (8)

Country Link
US (1) US7780808B2 (fr)
EP (1) EP1263572B1 (fr)
AT (1) ATE249921T1 (fr)
AU (1) AU2001233835A1 (fr)
DE (1) DE60100802T2 (fr)
ES (1) ES2202274T3 (fr)
GB (1) GB0003029D0 (fr)
WO (1) WO2001058680A1 (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DK1746284T4 (da) 2001-07-19 2021-10-18 Vestas Wind Sys As Vindmøllevinge
GB0117804D0 (en) 2001-07-21 2001-09-12 Bae Systems Plc Aircraft structural components
EP1544099B1 (fr) * 2003-12-18 2009-01-07 Airbus UK Limited Méthode pour joindre des éléments de structure d'avion
GB0329373D0 (en) 2003-12-18 2004-01-21 Airbus Uk Ltd Method of joining structural elements in an aircraft
ES2347507B1 (es) * 2007-12-27 2011-08-17 Airbus Operations, S.L. Boca de acceso de aeronave optimizada.
FR2933067B1 (fr) * 2008-06-26 2010-10-08 Airbus France Panneau de fuselage d'aeronef renforce et procede de fabrication.
CN102481971B (zh) * 2009-10-08 2014-12-31 三菱重工业株式会社 复合材料构造体、具备该构造体的航空器主翼及航空器机身
GB201000878D0 (en) 2010-01-20 2010-03-10 Airbus Operations Ltd Sandwich panel
CN101891015B (zh) * 2010-07-20 2013-04-10 中国航空工业集团公司西安飞机设计研究所 一种蒙皮板减重方法
US9108387B2 (en) * 2011-06-30 2015-08-18 The Boeing Company Electrically conductive structure
FR2977186B1 (fr) 2011-07-01 2014-08-22 Daher Aerospace Procede de renforcement local d'un panneau composite a renfort fibreux et panneau obtenu par un tel procede
ES2401520B1 (es) * 2011-07-28 2014-06-10 Airbus Operations S.L. procedimiento de fabricación de una pieza de material compuesto de un compartimento cerrado con una disposición de acceso integrada
GB201115080D0 (en) 2011-09-01 2011-10-19 Airbus Operations Ltd An aircraft structure
DE102011083162A1 (de) * 2011-09-21 2013-03-21 Bayerische Motoren Werke Aktiengesellschaft Mehrlagiges Faserverbundbauteil und Verfahren zum Herstellen desselben
WO2015008253A1 (fr) * 2013-07-19 2015-01-22 Philip Morris Products, S.A. Papier hydrophobe
EP2842865B1 (fr) * 2013-08-28 2019-12-18 Airbus Operations GmbH Panneau de fenêtre pour une cellule d'aéronef et son procédé de production
US10479517B2 (en) * 2016-12-05 2019-11-19 The Boeing Company Composite fan cowl with a core having tailored thickness
JP6770987B2 (ja) * 2018-03-12 2020-10-21 株式会社Ｓｕｂａｒｕ 複合材構造体、航空機及び雷電流の誘導方法
US11446884B2 (en) * 2018-10-29 2022-09-20 Airbus Operations Gmbh Process for producing a component which is two-dimensional in regions from a fibre composite material
GB2604126A (en) * 2021-02-24 2022-08-31 Airbus Operations Ltd Reinforced holes

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2154286A (en) 1984-02-13 1985-09-04 Gen Electric Hollow laminated airfoil
US5866272A (en) 1996-01-11 1999-02-02 The Boeing Company Titanium-polymer hybrid laminates
FR2771330B1 (fr) * 1997-11-26 2004-02-27 Aerospatiale Procede de fabrication d'un panneau composite monolithique articule avec des moyens raidisseurs integres, panneau articule obtenu et capot articule dans un aeronef
GB9826681D0 (en) 1998-12-04 1999-01-27 British Aerospace Composite laminates

Also Published As

Publication number Publication date
DE60100802D1 (de) 2003-10-23
US20030021958A1 (en) 2003-01-30
EP1263572A1 (fr) 2002-12-11
DE60100802T2 (de) 2004-04-08
EP1263572B1 (fr) 2003-09-17
WO2001058680A1 (fr) 2001-08-16
AU2001233835A1 (en) 2001-08-20
ATE249921T1 (de) 2003-10-15
ES2202274T3 (es) 2004-04-01
US7780808B2 (en) 2010-08-24

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Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)